@inproceedings{a0cf56a775684564823da05ca1c45100,
title = "Analytical statistics of forced response of a mistuned bladed disk assembly in subsonic flow",
abstract = "The statistics of the forced response of a structurally and aerodynamically coupled bladed disk assembly have been computed efficiently by the analytical technique. The validity of the analytical technique has been corroborated by comparison with the results from numerical simulations. Lastly, the effects of the following parameters on the statistics of the maximum amplitude have been studied: Aerodynamic coupling, fluid density, and stagger angle.",
author = "S. Chen and A. Sinha",
note = "Funding Information: This work has been supported by the AFOSR Grant 87-0142. Publisher Copyright: {\textcopyright} Copyright 1990 by ASME.; ASME 1990 International Gas Turbine and Aeroengine Congress and Exposition, GT 1990 ; Conference date: 11-06-1990 Through 14-06-1990",
year = "1990",
doi = "10.1115/90-GT-205",
language = "English (US)",
series = "Proceedings of the ASME Turbo Expo",
publisher = "American Society of Mechanical Engineers (ASME)",
booktitle = "Manufacturing Materials and Metallurgy; Ceramics; Structures and Dynamics; Controls, Diagnostics and Instrumentation; General",
}